发明授权
US06574965B1 Rotor tip bleed in gas turbine engines 有权
燃气轮机发动机转子尖端泄漏

  • 专利标题: Rotor tip bleed in gas turbine engines
  • 专利标题(中): 燃气轮机发动机转子尖端泄漏
  • 申请号: US09220468
    申请日: 1998-12-23
  • 公开(公告)号: US06574965B1
    公开(公告)日: 2003-06-10
  • 发明人: Matthew R. Feulner
  • 申请人: Matthew R. Feulner
  • 主分类号: F02C604
  • IPC分类号: F02C604
Rotor tip bleed in gas turbine engines
摘要:
A gas turbine engine includes a compressor, a combustor, and turbine enclosed in an engine case with the compressor having a plurality of alternating rows of rotating blades and stationary vanes. The gas turbine engine also includes a substantially circumferential groove formed in the engine case of the compressor section. The groove is substantially adjacent to a row of rotating blades to extract a portion of tip leakage flow from that row of blades and to route the extracted tip leakage flow to the turbine section for cooling turbine components. In the preferred embodiment of the present invention, the groove communicates with a plenum which communicates with the turbine section of the gas turbine engine via channeling pipes formed within the engine case.
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